Method of providing electric power with thermal protection

ABSTRACT

An electric machine including a magnetic component, forming part of its rotor or stator that loses its magnetic characteristics above a certain chosen temperature is disclosed. This magnetic material forms part of a magnetic circuit that guides flux about the stator. As a result, any magnetic flux emanating with the rotor stops circulating about the stator above this temperature, and the machine stops acting as generator. The component is thermally coupled to windings carrying current from the machine&#39;s stator. The material forming the component is selected so that the chosen temperature is lower than the temperature at which the machine would be thermally damaged. This, in turn, limits the operating temperature of the windings, and thus prevents overheating of the machine during operation, typically caused by a fault. Preferably this magnetic material is formed from a ferrite material, such as a Manganese Zinc ferrite material.

CROSS-REFERENCE TO RELATED APPLICATIONS

[0001] This application is a continuation of application Ser. No. 09/949,855, which is a divisional application of Ser. No. 09/467,761, now U.S. Pat. No. 6,313,560.

FIELD OF THE INVENTION

[0002] The present invention relates to electric machines, and more particularly to electric generators that are thermally protected from damage resulting from high currents in such machines.

BACKGROUND OF THE INVENTION

[0003] Permanent magnet electric motors and generators are well known and understood. Typically, such permanent magnet machines include a rotor formed, at least in part, from a magnetic material such as Samarium-Cobalt. Electric windings on a stator about the rotor are used to carry current that either generates a magnetic field or is the result of a magnetic field about the rotor. As a motor, current through the windings induces the rotating magnetic field, which in turn applies a torque to the magnetic portion of the rotor causing it to act as motor. Similarly, as a generator, torque applied to the rotor, results in a rotating magnetic field that induces a current in the windings.

[0004] Such electric machines provide significant benefits over synchronous machines, squirrel cage motors and other types of electric machines. Significantly, permanent magnet machines do not require brushes; are relatively light; use conventional and developed electronics to generate any required rotating magnetic field; and can act as both motors and generators.

[0005] In view of these benefits, such machines appear well suited for aircraft applications. Particularly, such machines would appear to lend themselves for use as starters and generators within a turbine engine.

[0006] Conveniently, such machines can be connected directly to the engine shaft. When required, generated electricity can be rectified and filtered using conventional lightweight electronics. When DC currents are required, as in traditional aircraft applications, the speed of rotation and frequency of generator output does not need be controlled. Heavy gearing is therefore not required. Operating as motors, such machines can act as starters.

[0007] Disadvantageously, however, machines coupled to such engines can potentially generate extreme power limited only by the power of the turbine engine driving the rotor of the machine. Unabated, generation of such electric power can result in extreme heat, particularly in the stator windings, that may cause the motor to melt and potentially burn. This is clearly undesirable. Obviously, current provided by the machine to interconnected electrical equipment may be limited by fusing the interconnected equipment or even the electronics used to rectify or regulate AC currents. However, such fusing will not react to short circuits internal to the machine. While unlikely, such short circuits might, for example, occur in the stator windings. Should this happen, a permanent magnet machine will invariably overload and overheat causing damage to the machine, and perhaps even to the associated engine. In the extreme case, this may cause the main engine to fail as a result of the high temperature of the engine shaft coupled to the motor. Similar problems may be manifested in other types of electric machines.

[0008] Accordingly, an improved electric machine that is thermally protected is desirable.

SUMMARY OF THE INVENTION

[0009] In accordance with the present invention, an electric machine includes a ferrite portion, forming part of its rotor or stator that loses its magnetic characteristics above a certain chosen temperature. As a result, any magnetic flux circulating between the rotor and stator is significantly reduced above this temperature, and the machine stops acting as generator. The component is thermally coupled to windings carrying current from the machine's stator. The material forming the component is selected so that the certain temperature is lower than the temperature at which the machine would be thermally damaged. This, in turn, limits the operating temperature of the windings, and thus preventing overheating of the machine during operation.

[0010] In accordance with an aspect of the present invention an electric machine includes a permanent magnet motor and a stator mounted about the rotor, at least partially forming a magnetic circuit guiding a magnetic flux emanating from the permanent magnet. At least one winding extends about the stator for picking up a current induced by the magnetic flux. At least a portion of the magnetic circuit is thermally coupled to the winding and is formed from magnetic material having a Curie temperature below a temperature at which the machine is damaged. This limits the magnetic flux about the magnetic circuit above the Curie temperature, and thus limits the operating temperature of the windings, and prevents overheating of the machine during operation.

[0011] In accordance with another aspect of the invention, an electric generator includes a rotor assembly including a permanent magnet; and a stator formed of a ferrite material mounted about the rotor, at least partially forming a magnetic circuit guiding a magnetic field emanating from the permanent magnet. At least one winding extends about the stator for picking up a current induced by the magnetic field. Preferably, the ferrite material is a Manganese-Zinc ferrite material.

[0012] Other aspects and features of the present invention will become apparent to those of ordinary skill in the art, upon review of the following description of specific embodiments of the invention in conjunction with the accompanying figures.

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] In figures which illustrate, by way of example only, preferred embodiments of the invention,

[0014]FIG. 1 is an exploded view of a permanent magnet machine, exemplary of an embodiment of the present invention;

[0015]FIG. 2 is a cross sectional view of the machine of FIG. 1;

[0016]FIG. 3 is an exploded view of a partial stator assembly that may form part of the machine of FIG. 1;

[0017]FIG. 4 is a side perspective view of an exemplary stator assembly forming part of the machine of FIG. 1;

[0018]FIG. 5 is a back end view of FIG. 4;

[0019]FIG. 6 is a front end view of FIG. 4;

[0020]FIG. 7 schematically illustrates the flow of current about the stator assembly of FIG. 4; and

[0021]FIG. 8 is a top view of a portion of a further stator that may be used with a machine exemplary of a further embodiment of the present invention; and

[0022]FIG. 9 shows a gas turbine engine incorporating the present invention, with a portion of the engine broken away to reveal a cross-section thereof.

DETAILED DESCRIPTION

[0023]FIGS. 1 and 2 illustrate a permanent magnet electric machine 10, exemplary of an embodiment of the present invention. As illustrated, electric machine 10 includes a stator assembly 12 and rotor assembly 14, preferably mounted within a housing 16. Rotor assembly 14 is mounted for free rotation about its central axis within housing 16 by bearings 20 and 22.

[0024] Housing 16 includes an outer cylindrical shell 24, and generally disc shaped front and rear end plates 26 and 28. End plates 26 and 28 are fixed to shell 24, and thereby retain stator assembly 12, rotor assembly 14, and bearings 20 and 22 within housing 16. Annular walls 30 and 32 extend inwardly from the interior of end plates 26 and 28 and retain bearings 20 and 22 at defined axial positions within housing 16, about rotor assembly 14. A further retaining washer 23 assists to retain bearings 20 and 22. Housing 16 is preferably formed of high-grade stainless steel.

[0025] Example rotor assembly 14 includes a generally cylindrical core section 38. Two smaller diameter cylindrical shafts 34 and 36 extend axially outward from core section 38, toward the front and rear of housing 16, respectively. Spacing ledges 42, 44 and 46, 48 separate shafts 34 and 36, respectively, from core section 38. Ledges 42 and 46 abut with bearings 20 and 22. A further smaller diameter concentric drive shaft 40 extends axially outward from shaft 34 and the front of housing 16. As will be appreciated, core section 38; shafts 34, 36 and 40 are preferably machined from a single piece of relatively low strength magnetic steel, such as maraging steel. A thin shell 18 formed of non-magnetic material, such as a Nickle alloy, at least partially encapsulates core section 38 and contains the relatively low strength magnetic steel. Shell 18 is preferably formed of AMS 5662 or AMS 5663 Nickel Alloy and may be shrink fitted to the core portion 38 and then ground to achieve a desired overall thickness of shell 18.

[0026] Stator assembly 12 is further illustrated in FIGS. 3-7. As illustrated, stator assembly 12 includes a magnetic circuit defined by an exemplary hollow cylinder 50. Cylinder 50 includes a plurality of lengthwise extending, evenly spaced slots 52 a, 52 b and 52 c (collectively slots 52) extending on its interior. In the preferred embodiment, a total of eighteen such slots extend along the cylinder's length. Conveniently, the eighteen slots 52 a, 52 b and 52 c may be grouped into three groups, with all slots 52 a belonging to one group, all slots 52 b and 52 c to another. Each third slot belongs in one of the groups. As best illustrated in FIG. 3, a set of six rectangular conductors 54 a that are complementary in shape to slots 52 a, occupy the entire length of these slots. Each of these conductors is formed of a material such as copper, and is insulated by a thin plastic coating. Each of conductors 54 a is identical in length, and extends slightly beyond the ends of cylinder 50. Adjacent conductors within the group of conductors 54 a are interconnected by arced conductors 56 a extending radially about the central axis of cylinder 50, and exterior to cylinder 50. Alternating pairs of conductors 54 a are connected at opposite ends of cylinder 50. Thus, two arced conductors 56 a are at one end of cylinder 50 and three are at the opposite. Conductors 54 a and 56 a thus form an electric circuit (referred to as circuit 58 a) traversing the length of cylinder 50 six times, at intervals spaced sixty degrees about a central axis of cylinder 50. Diametrically opposed rectangular conductors (ie. spaced by one-hundred and eighty degrees) have currents running in opposite direction along the length of cylinder 50 and thus form current loops or windings about the central axis of machine 10. As illustrated in FIGS. 4-6, conductors 54 b, 56 b and 54 c, 56 c are similarly arranged to occupy the remaining slots 52 b and 52 c, and thus form circuits 58 b and 58 c. Resulting circuits 58 a, 58 b and 58 c (collectively circuits 58) thus form nine current loops or windings about central axis of machine 10. As illustrated in FIG. 6, conductors 54 b and 54 c have the same length as conductors 54 a and are arranged at axial positions so that conductors 54 a, 54 b, 54 c (collectively conductors 54) and 56 a, 56 b and 56 c (collectively conductors 56) are not in contact with each other. Moreover, these conductors are preferably insulated so that they are not electrically connected with cylinder 50, and are thermally coupled to cylinder 50. The conductors may be coupled to cylinder 50 by way of a known thermal conductive varnish or epoxy. Cylinder 50 and conductors 54 may be encapsulated using this varnish or epoxy. Contact points for each circuit 58 a, 58 b and 58 c extend from the rear end of cylinder 50, as illustrated in FIG. 5. Current flow in circuits 58 a, 58 b and 58 c as viewed at the rear of machine 10, resulting from a potential difference across the contact points is schematically illustrated in FIG. 7.

[0027] As illustrated, stator assembly 12 and cylinder 50 are coaxial with core section 38. A small air gap separates core section 38 from cylinder 50.

[0028] A conventional three phase circuit (not shown) may be used to drive circuits 58 a, 58 b and 58 c to cause machine 10 to act as a motor. Specifically, driving circuits 58 results in a rotating magnetic field generated by the nine windings or current loops, travelling circumferentially within cylinder 50. This field is guided by cylinder 50 acting as part of a magnetic circuit about the center axis of this cylinder 50, and in turn the core section 38 of rotor assembly 14. As will be appreciated by those of ordinary skill in the art, the rotating magnetic field exerts a torque on the magnetic portion of rotor assembly 14, causing it to rotate.

[0029] Cylinder 50 is preferably formed of a ferrite material. As is understood by those of ordinary skill in the art, ferrite materials exhibit magnetic properties and have high relative permeability resulting in low magnetic reluctance, allowing such materials to guide magnetic flux. Ferrites typically have cubic crystalline structure with the chemical formula MO.Fe₂O₃, where MO is typically a combination of two or more divalent metals, such as zinc, nickel, manganese or copper. Ferrites are typically classified as “hard” or “soft”. “Soft” ferrite materials only exhibit significant magnetic characteristics in the presence of a magnetic field, while “hard” ferrite materials tend to permanently retain their magnetic characteristics. As is further, understood, the nature of most magnetic materials is typically temperature dependent. Most magnetic materials lose their magnetic properties above a critical temperature, referred to as the Curie temperature of the material. For many materials, and for most ferrites, once the temperature of the material drops below the critical temperature, their magnetic properties return. Iron, for example, has a Curie temperature of about 770° C. In fact, most magnetic materials used in electric machines have Curie temperature far exceeding the operating temperature of the machine. In machine 10, however, cylinder 50 and hence the magnetic circuit defined by cylinder 50 is formed of a material (preferably a ferrite) having a Curie temperature above conventional operating temperatures, but below a critical temperature at which damage might be caused to the circuits 58 or the remainder of machine 10. For reasons that will become apparent, this Curie temperature may be considered to be the desired shut-down temperature of machine 10. Preferably, cylinder 50 is formed of a “soft” ferrite having a Curie temperature of approximately 200° C. A ferrite having such property is, for example, a Manganese-Zinc available from Phillips under material type 3C85, having a Curie temperature of 215° C. Of course, other materials may be suitable, and will be easily identified by those of ordinary skill in the art. Preferably the material will have a Curie temperature between 95° C. and 300° C. depending on the desired shut-down temperature. Of course, some machine designs may require lower or higher shut-down temperatures.

[0030] In operation then, circuits 58 may be driven by a three-phase power source, as describe above, causing machine 10 to act as a motor. Instead of using an alternating current three-phase power source, each of circuits 58 a, 58 b and 58 c may be driven by a square wave source, with each square way source out of phase with another square wave source by 120°. As will be appreciated, this has the same effect of using a poly-phase AC source, driving rotor assembly 14.

[0031] More significantly, however, machine 10 may be operated as a generator by driving shaft 40 using a rotational source of mechanical power. For example, shaft 40 may be interconnected with the power shaft of a gas turbine engine, and driven at very high speeds (potentially in excess of 100,000 rpm). As will be appreciated, rotating rotor assembly 14, and more particularly magnetic shell 18 will generate a rotating magnetic field about the central axis of rotor assembly 14. This, in turn, establishes an alternating magnetic flux in the magnetic circuit defined by cylinder 50. This flux, in turn, induces an electric current in the windings defined by circuits 58 a, 58 b and 58 c. As will be appreciated, the current so generated will be three-phase current, having a frequency proportional to the speed of rotation of rotor assembly 14, with current through circuits 58 a, 58 b and 58 c being out of phase with each other by 120°. If desired, this current may be rectified using a conventional rectification circuit (also not shown).

[0032] Now, in the event machine 10 is subject to an internal fault, such as for example, caused by a short across conductors 54 or 56, current in the conductors will increase, resulting in increased heat in the conductors. Moreover, as conductors 54, and 56 are preferably in physical contact with, and thermally coupled to cylinder 50, increase in temperature of conductors 54 or 56 will be transferred to cylinder 50. As the temperature of cylinder 50 approaches the Curie temperature of the material forming cylinder 50, cylinder 50 loses its magnetic properties, thereby severely limiting the flux through cylinder 50 and the current induced in the windings formed by circuits 58, and effectively shutting down machine 10 acting as a generator. Clearly, as the current is reduced, the temperature of the conductors is reduced until the temperature of cylinder 50 again drops below the Curie temperature of the material and its magnetic properties return. As will be apparent, in steady state and in the presence of a fault, machine 10 will operate with cylinder 50 at or near the selected shut-down or Curie temperature. Clearly, for a properly chosen Curie temperature, cylinder 50 acts as temperature activated fuse, limiting the operating temperature of machine 10, and thereby any damage to its components.

[0033] Additionally, the use of ferrite material in the formation of stator assembly 12 advantageously reduces Hysteresis and Eddy current losses within stator assembly 12. This becomes particularly beneficial at high speeds.

[0034] In yet another embodiment, rotor assembly 14 may include a material having the desired shut-down Curie temperature. Preferably, a ferrite material is placed radially outward of magnets forming part of rotor assembly 14, effectively as part of the magnetic circuit formed coupling the flux from rotor assembly 14 to stator assembly 12. Cylinder 50 may be formed of a material having a much higher Curie temperature. The ferrite material on rotor assembly 14 may then be thermally coupled to the conductors forming circuits 58. These conductors, could for example, be coupled to rotor assembly 14 by radiation or convection. In the event that the temperature of these conductors increases, the increase in temperature is conducted to the ferrite portion of the rotor assembly 14, thereby causing the ferrite material to lose its magnetic properties near the Curie temperature. This results in a portion of the magnetic circuit about the magnets of rotor assembly 14 having a very low permeability, thereby reducing the magnetic flux emanating with rotor assembly and coupled to cylinder 50; the resulting flux in cylinder 50; and the resulting current in circuits 58. Again, at steady state this second embodiment will operate with the temperature of the windings and rotor at or near the selected shut-down or Curie temperature.

[0035] In a further embodiment, a cylinder 50′ illustrated in FIG. 8 may form part of a machine that is otherwise identical to machine 10, may be formed of more than one material. A portion 62 of the cylinder 50, of cylinder 50 is preferably formed of ferrite material having the desired shut-down Curie temperature, and the remaining portion 64 of the cylinder formed of a material having a different Curie temperature. For example the toothed portion (ie. the lengthwise extending teeth or ridges) of cylinder 50′ may be formed of laminated iron, while the remainder may be formed of Manganese-Zinc having a Curie temperature of about 200° C. Individual iron teeth or ridges may be epoxied to a Manganese-Zinc portion. Above the Curie temperature, the resulting magnetic circuit would have a very high reluctance, severely limiting the magnetic flux guided about rotor assembly 14, and therefore the current through windings about the cylinder 50′, again causing cylinder 50′ to operate at or near the chosen Curie temperature. Of course, other configurations of cylinder 50′ having other portions formed of a magnetic material having the desired Curie temperature will be readily apparent to those of ordinary skill in the art.

[0036] Clearly, the above embodiments may be modified in many ways while still embodying the invention. For example, the shape of cylinder 50 could be modified—a toroid or other shape could take its place; the arrangements of conductors and windings could be changed in any number of known ways; the permanent magnet of rotor assembly 14 can be formed in numerous ways; and the size of the machine can be scaled (increased or decreased) as required; other magnetic materials having suitable Curie temperature may be used. Thus it is apparent that the described invention may be embodied in many ways. As further examples, the invention could be embodied in a salient pole DC machine; or in a synchronous machine.

[0037] The present invention is particularly well suited, among other things, to prevent overheating problems of an internally short circuited permanent magnet arrangement that is driven continuously. For example, as depicted in FIG. 9, in the case of an internal fault in a machine 70 driven by a shaft 71 in gas turbine engine 72. The invention also permits a certain level of control to be attained over an alternator which is driven at variable speeds (i.e. driven by an operating propulsive aircraft gas turbine).

[0038] The above described embodiments, are intended to be illustrative only and in no way limiting. The described embodiments of carrying out the invention, are susceptible to many modifications of form, size, arrangement of parts, and details of operation. The invention, rather, is intended to encompass all such modification within its scope, as defined by the claims. 

11. (Previously Presented) A method of thermally protecting an electric generator to prevent overheating, said generator comprising a stator mounted about a rotor, and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising: forming at least a portion of said magnetic circuit from magnetic material having a Curie temperature below a temperature at which said generator is damaged; thermally coupling said winding to said portion of said magnetic circuit, so that said magnetic circuit limits flow of said magnetic flux about said magnetic circuit above said Curie temperature, limiting operating temperature of said windings, and preventing overheating of said generator during operation.
 12. (Previously Presented) The method of claim 11, further comprising choosing said portion of said magnetic material to have a Curie temperature between 95 and 300 degrees Celsius.
 13. (Previously Presented) The method of claim 12, wherein said portion of said magnetic circuit is formed from a Manganese-Zinc ferrite material.
 14. (Previously Presented) The method of claim 11, further comprising providing a thermally conductive compound between said stator and said windings to thermally couples said winding to said stator.
 15. (Previously Presented) A method of providing a thermally limited source of electrical power within an aircraft, said method comprising: providing an electric generator comprising a stator mounted about a rotor, and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, wherein said magnetic circuit comprises a portion formed from magnetic material having a Curie temperature below a temperature at which said generator is damaged; and said stator is thermally coupled to said winding, so that said magnetic circuit is thermally coupled to said winding and thereby limits flow of said magnetic flux about said magnetic circuit above said Curie temperature, limiting operating temperature of said windings, and preventing overheating of said generator during operation; driving said rotor using an engine of said aircraft to generate electrical power from said generator.
 16. (Previously Presented) The method of claim 15, further comprising heating said windings above said Curie temperature in the presence of a short circuit, thereby heating said portion and limiting flow of said magnetic flux about said magnetic circuit above said Curie temperature, thereby limiting operating temperature of said windings, and preventing overheating of said generator during operation.
 17. (Previously Presented) The method of claim 16, wherein said heating comprising heating said portion above 95 degrees Celsius to limit flow of magnetic flux about said magnetic circuit.
 18. (Previously Presented) The method of claim 17, wherein said heating comprises heating said portion below 300 degrees Celsius to limit flow of magnetic flux about said magnetic circuit.
 19. (Previously Presented) A method of preventing overheating in an electric generator in the presence of an internal fault, said generator having a stator, a rotor and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising: (a) determining a desired shut-down temperature for said generator which is below a temperature at which said generator is thermally damaged; and (b) selecting a generator having at least a portion of said magnetic circuit composed of a magnetic material having a Curie temperature substantially equal to said desired shut-down temperature, said winding being thermally coupled to said portion of said magnetic circuit, so that in the presence of an internal fault causing an operating temperature of said windings to increase, said portion of said magnetic circuit is heated to said Curie temperature, thereby limiting said magnetic flux about said magnetic circuit and current induced in said windings, and thereby preventing overheating of said generator in the presence of said internal fault.
 20. (Previously Presented) The method of claim 19, wherein said shut-down temperature is below 300 degrees Celsius.
 21. (Previously Presented) The method of claim 19, wherein said portion is formed on said stator.
 22. (Previously Presented) A method of preventing overheating in an electric generator, said generator having a stator, a rotor and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising: (a) determining a desired shut-down temperature for said generator which is below a temperature at which said generator is damaged; and (b) selecting a generator having at least a portion of said magnetic circuit composed of a magnetic material having a Curie temperature not greater than said desired shut-down temperature, said winding being thermally coupled to said portion of said magnetic circuit, so that an increase in operating temperature of said windings causing said portion of said magnetic circuit to increase to said Curie temperature thereby limits said magnetic flux about said magnetic circuit and current induced in said windings, thereby substantially shutting down an electricity generating function of said generator until said portion of said magnetic circuit cools below said Curie temperature.
 23. (Previously Presented) The method of claim 22, wherein said shut-down temperature is below 300 degrees Celsius.
 24. (Previously Presented) The method of claim 22, wherein said portion is formed on said rotor.
 25. (Previously Presented) A method of providing a thermally limited source of electrical power within an aircraft, said method comprising: (a) determining a desired shut-down temperature for a generator, (b) selecting a generator having a stator, a rotor and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, at least a portion of said magnetic circuit composed of a magnetic material having a Curie temperature not greater than said desired shut-down temperature, said winding being thermally coupled to said portion of said magnetic circuit; (c) in the presence of an unintended short circuit in said windings, permitting an increase in an operating temperature of said windings to thereby cause said portion of said magnetic circuit to increase in temperature; and (d) permitting said portion of said magnetic circuit to increase in temperature to said Curie temperature thereof to thereby limit said magnetic flux about said magnetic circuit and current induced in said windings, thereby shutting down an electricity generating function of said generator. 